[list_settings.list_name] Current STS TLEs @ 12:30 UTC
Date:
May 17th 2011
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2011/136/12:56:27 958 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 52 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 0
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
136/15:49:35
292 46
0 93
0 93
0
000/02:53:07
333 36
8 0
0 177
3
000/00:01:01
779 71
9 -0
0 175
4
137/06:22:27
893 -0
6 11
1 11
1
000/17:25:59
935 -7
8 -0
0 181
9
000/00:00:16
735 -7
9 -0
0 176
7
137/15:45:28
881 3
0 3
0 3
4
001/02:49:00
922 -1
1 1
6 183
2
000/00:00:14
959 -1
0 0
0 176
6
138/06:06:43
785 -3
7 7
4 7
4
001/17:10:15
827 6
1 0
0 183
3
000/00:00:32
198 1
9 0
0 180
9
138/07:38:19
921 -4
7 8
9 8
9
001/18:41:51
963 7
3 -0
1 185
8
000/00:00:13
926 2
2 0
0 182
8
138/08:55:13
017 -0
4 2
4 2
8
001/19:58:45
059 2
3 0
0 187
1
000/00:00:12
118 1
5 1
4 183
1
Coasting Arc #1 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2011/136/13:37:08
240
Vector Time (MET): 000/00:40:40
282
Weight (LBS) : 249795
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5328475
02 A = 6662590
97 meter
Y = 3908010
78 meter E =
0079606
Z = -168916
42 I = 51
45510
XDOT = -2755
616516 Wp = 173
39633
YDOT = -4005
278533 meter/sec RA = 322
57596 deg
ZDOT = -6094
320475 TA = 8
47602
MA = 8
34236
Ha = 175
753 n
mi
Hp = 124
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17481873
43 X = -5370958
54
Y = 12821557
67 feet Y = 3848187
01 meter
Z = -554187
74 Z = -194905
51
XDOT = -9040
736600 XDOT = -2681
018247
YDOT = -13140
677602 feet/sec YDOT = -4035
675885 meter/sec
ZDOT = -19994
489747 ZDOT = -6107
526657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8706417
37 X = 2653716
02
Y = 19851414
93 feet Y = 6050711
27 meter
Z = -659534
42 Z = -201026
09
XDOT = -13321
619421 XDOT = -4060
429599
YDOT = 5209
058412 feet/sec YDOT = 1587
721004 meter/sec
ZDOT = -20047
713540 ZDOT = -6110
543087
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11136
59836744
00020000 00000-0 20000-3 0 9005
2 00134 51
6415 322
9779 0070340 179
7585 180
3638 15
98793620 28
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11136
59836744 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 322
9779 deg
Eccentricity:
0070340
Arg of perigee: 179
7585 deg
Mean anomaly: 180
3638 deg
Mean motion: 15
98793620 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 285
Coasting Arc #2 (Orbit 2)
---------------------------------------
Vector Time (GMT): 2011/136/15:50:06
181
Vector Time (MET): 000/02:53:38
223
Weight (LBS) : 247506
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4966618
14 A = 6711232
97 meter
Y = -4464347
28 meter E =
0010902
Z = -588602
82 I = 51
45491
XDOT = 3620
388049 Wp = 343
02227
YDOT = 3234
893051 meter/sec RA = 322
07529 deg
ZDOT = 5995
729488 TA = 10
53229
MA = 10
50947
Ha = 177
295 n
mi
Hp = 175
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16294678
93 X = 5019029
57
Y = -14646808
66 feet Y = -4408514
44 meter
Z = -1931111
60 Z = -564347
61
XDOT = 11877
913545 XDOT = 3554
819056
YDOT = 10613
166179 feet/sec YDOT = 3275
011281 meter/sec
ZDOT = 19671
028504 ZDOT = 6013
158684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19474055
01 X = -5935691
97
Y = -10058675
98 feet Y = -3065884
44 meter
Z = -1832751
02 Z = -558622
51
XDOT = 5025
447082 XDOT = 1531
756271
YDOT = -13337
509248 feet/sec YDOT = -4065
272819 meter/sec
ZDOT = 19741
377091 ZDOT = 6017
171737
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11136
66086709
00020000 00000-0 20000-3 0 9012
2 00134 51
6444 322
6453 0010531 281
2578 78
7405 15
81339621 35
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11136
66086709 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 322
6453 deg
Eccentricity:
0010531
Arg of perigee: 281
2578 deg
Mean anomaly: 78
7405 deg
Mean motion: 15
81339621 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3
Checksum: 249
Coasting Arc #3 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2011/137/06:22:36
261
Vector Time (MET): 000/17:26:08
303
Weight (LBS) : 247232
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5745303
95 A = 6715005
13 meter
Y = 2643930
70 meter E =
0013569
Z = -2231264
05 I = 51
43428
XDOT = -379
255222 Wp = 226
60144
YDOT = -5439
230710 meter/sec RA = 318
95137 deg
ZDOT = -5457
179757 TA = 338
58128
MA = 338
63801
Ha = 181
916 n
mi
Hp = 176
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18849422
41 X = -5763602
62
Y = 8674313
31 feet Y = 2579581
14 meter
Z = -7320420
13 Z = -2259219
40
XDOT = -1244
275664 XDOT = -291
894059
YDOT = -17845
245112 feet/sec YDOT = -5442
982734 meter/sec
ZDOT = -17904
133060 ZDOT = -5458
810581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20604531
20 X = -6280261
11
Y = -2080142
84 feet Y = -634027
54 meter
Z = -7433659
07 Z = -2265779
28
XDOT = 7933
625010 XDOT = 2418
168903
YDOT = -14447
493544 feet/sec YDOT = -4403
596032 meter/sec
ZDOT = -17910
450160 ZDOT = -5459
105209
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11137
29283697
00020000 00000-0 20000-3 0 9028
2 00134 51
6454 319
3700 0014865 250
5426 109
4134 15
79260175 135
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11137
29283697 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 319
3700 deg
Eccentricity:
0014865
Arg of perigee: 250
5426 deg
Mean anomaly: 109
4134 deg
Mean motion: 15
79260175 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 255
Coasting Arc #4 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2011/137/15:45:36
360
Vector Time (MET): 001/02:49:08
402
Weight (LBS) : 247135
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2889581
43 A = 6706582
33 meter
Y = -3026627
76 meter E =
0005227
Z = -5239854
87 I = 51
39077
XDOT = 5607
640942 Wp = 194
41404
YDOT = -5291
768851 meter/sec RA = 316
90196 deg
ZDOT = -40
773593 TA = 75
22717
MA = 75
16926
Ha = 183
247 n
mi
Hp = 176
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9480254
05 X = -2830067
67
Y = -9929881
09 feet Y = -3058607
45 meter
Z = -17191124
90 Z = -5253748
47
XDOT = 18397
772121 XDOT = 5666
595814
YDOT = -17361
446360 feet/sec YDOT = -5228
731168 meter/sec
ZDOT = -133
771630 ZDOT = -13
388637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5994480
12 X = -1827117
54
Y = 12272470
14 feet Y = 3740648
90 meter
Z = -17247179
92 Z = -5256940
44
XDOT = -21831
492978 XDOT = -6654
239060
YDOT = -10672
567355 feet/sec YDOT = -3252
998530 meter/sec
ZDOT = -22
701833 ZDOT = -6
919519
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11137
67249943
00020000 00000-0 20000-3 0 9037
2 00134 51
6444 317
4056 0017199 252
9243 107
0039 15
78749968 198
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11137
67249943 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 317
4056 deg
Eccentricity:
0017199
Arg of perigee: 252
9243 deg
Mean anomaly: 107
0039 deg
Mean motion: 15
78749968 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 19
Checksum: 287
Coasting Arc #5 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2011/138/06:06:59
884
Vector Time (MET): 001/17:10:31
926
Weight (LBS) : 246924
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335070
52 A = 6711659
58 meter
Y = 1229198
26 meter E =
0008341
Z = 4981267
56 I = 51
38223
XDOT = -3970
190080 Wp = 231
16496
YDOT = 6320
846735 meter/sec RA = 313
81732 deg
ZDOT = 1892
363468 TA = 200
48607
MA = 200
51955
Ha = 183
298 n
mi
Hp = 180
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14222672
30 X = 4296804
77
Y = 4032802
69 feet Y = 1277461
06 meter
Z = 16342741
35 Z = 5002234
83
XDOT = -13025
558005 XDOT = -4049
768806
YDOT = 20737
686138 feet/sec YDOT = 6276
004471 meter/sec
ZDOT = 6208
541562 ZDOT = 1872
883529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9561042
17 X = 2914205
65
Y = 11151523
60 feet Y = 3398984
39 meter
Z = 16427510
27 Z = 5007105
13
XDOT = -21517
278018 XDOT = -6558
466340
YDOT = 9404
471065 feet/sec YDOT = 2866
482781 meter/sec
ZDOT = 6129
398924 ZDOT = 1868
240792
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11138
30554486
00020000 00000-0 20000-3 0 9040
2 00134 51
6451 314
1361 0011296 260
0568 99
9322 15
77374519 291
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11138
30554486 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 314
1361 deg
Eccentricity:
0011296
Arg of perigee: 260
0568 deg
Mean anomaly: 99
9322 deg
Mean motion: 15
77374519 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 263
Coasting Arc #6 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2011/138/07:38:26
884
Vector Time (MET): 001/18:41:58
926
Weight (LBS) : 246706
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4289196
71 A = 6716331
89 meter
Y = 1288709
90 meter E =
0002844
Z = 5005858
77 I = 51
38146
XDOT = -4010
669073 Wp = 179
51184
YDOT = 6323
949900 meter/sec RA = 313
48823 deg
ZDOT = 1805
631516 TA = 253
01444
MA = 253
04561
Ha = 185
784 n
mi
Hp = 182
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14072167
70 X = 4250149
46
Y = 4228050
86 feet Y = 1336455
34 meter
Z = 16423421
17 Z = 5026601
28
XDOT = -13158
363101 XDOT = -4089
858154
YDOT = 20747
867127 feet/sec YDOT = 6278
657164 meter/sec
ZDOT = 5923
987914 ZDOT = 1785
955887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12965565
92 X = 3951904
49
Y = 6710809
04 feet Y = 2045454
59 meter
Z = 16507277
88 Z = 5031418
30
XDOT = -16273
195964 XDOT = -4960
070130
YDOT = 17042
696151 feet/sec YDOT = 5194
613787 meter/sec
ZDOT = 5844
053160 ZDOT = 1781
267403
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11138
36896601
00020000 00000-0 20000-3 0 9055
2 00134 51
6460 313
8100 0004394 273
6227 86
4435 15
75691668 304
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11138
36896601 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 313
8100 deg
Eccentricity:
0004394
Arg of perigee: 273
6227 deg
Mean anomaly: 86
4435 deg
Mean motion: 15
75691668 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 261
Coasting Arc #7 (Orbit 30)
---------------------------------------
Vector Time (GMT): 2011/138/08:55:19
076
Vector Time (MET): 001/19:58:51
118
Weight (LBS) : 246627
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5250752
30 A = 6727682
08 meter
Y = -3952143
26 meter E =
0012369
Z = 1404943
73 I = 51
41343
XDOT = 1960
556293 Wp = 44
40885
YDOT = 4675
430390 meter/sec RA = 313
21055 deg
ZDOT = 5802
836071 TA = 331
10373
MA = 331
17216
Ha = 187
083 n
mi
Hp = 183
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17226877
62 X = 5287730
62
Y = -12966349
29 feet Y = -3893219
59 meter
Z = 4609395
44 Z = 1430541
53
XDOT = 6432
271302 XDOT = 1879
939534
YDOT = 15339
338551 feet/sec YDOT = 4696
903018 meter/sec
ZDOT = 19038
176085 ZDOT = 5812
165359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15028459
85 X = 4580674
56
Y = -15429500
69 feet Y = -4702911
81 meter
Z = 4713168
35 Z = 1436573
71
XDOT = 7451
008320 XDOT = 2271
067336
YDOT = 13105
858854 feet/sec YDOT = 3994
665779 meter/sec
ZDOT = 19075
679748 ZDOT = 5814
267187
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11138
43240352
00020000 00000-0 20000-3 0 9060
2 00134 51
6449 313
4829 0004098 299
2110 60
8644 15
75268101 312
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11138
43240352 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 313
4829 deg
Eccentricity:
0004098
Arg of perigee: 299
2110 deg
Mean anomaly: 60
8644 deg
Mean motion: 15
75268101 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 31
Checksum: 244
Coasting Arc #8 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2011/139/08:55:49
217
Vector Time (MET): 002/19:59:21
259
Weight (LBS) : 246627
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1484635
32 A = 6718136
74 meter
Y = -4405712
40 meter E =
0008342
Z = -4857157
62 I = 51
36058
XDOT = 5823
911073 Wp = 98
25772
YDOT = -4481
799220 meter/sec RA = 308
01246 deg
ZDOT = 2287
274962 TA = 194
09360
MA = 194
11689
Ha = 187
149 n
mi
Hp = 182
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4870850
77 X = -1411664
09
Y = -14454437
01 feet Y = -4421905
81 meter
Z = -15935556
51 Z = -4864193
40
XDOT = 19107
319793 XDOT = 5862
483313
YDOT = -14704
065682 feet/sec YDOT = -4416
457362 meter/sec
ZDOT = 7504
182945 ZDOT = 2315
660804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7178526
47 X = -2188014
87
Y = -13424746
83 feet Y = -4091862
83 meter
Z = -15963797
43 Z = -4865765
46
XDOT = 15285
584980 XDOT = 4659
046302
YDOT = -17225
440712 feet/sec YDOT = -5250
314329 meter/sec
ZDOT = 7619
267796 ZDOT = 2322
352824
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 00134U 11139
38397655
00020000 00000-0 20000-3 0 9075
2 00134 51
6442 308
5863 0004173 303
7568 56
3198 15
75314387 468
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11139
38397655 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 308
5863 deg
Eccentricity:
0004173
Arg of perigee: 303
7568 deg
Mean anomaly: 56
3198 deg
Mean motion: 15
75314387 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 46
Checksum: 285
SPACE SHUTTLE ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/STSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
Shuttle TLE list
Privacy Policy:
Private list